Download BLUE SKY SAT 6.5 ACTIVE SATELLITE Installation manual

Sky Connect Aviation Series
Installation Manual
Executive, FlightDeck, Classic
Revision # 5.0
Dated: March 24, 2007
Part Number 1616-950-5.0
Revision Date: March 24, 2007
Revision 5.0
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Revision Date: March 24, 2007
Revision 5.0
TABLE of CONTENTS
LIST OF REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii
INDEX OF ACRONYMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv
GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SYSTEM DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TECHNICAL SPECIFICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1-1
1-1
1-1
1-2
INSTALLATION PROCESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SIM CARD ACTIVATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ANTENNA PLACEMENT PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INFORMATION NEEDED FOR CONFIGURATION . . . . . . . . . . . . . . . . . . . . . . .
WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2-1
2-1
2-1
2-1
2-1
2-1
INSTALLATION - GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1
A DISCUSSION ON SIM CARDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1
ITEMS REQUIRED BUT NOT SUPPLIED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 2
GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS . . . . . . 3 - 3
SYSTEM COMPONENTS THAT APPLY ONLY TO EXECUTIVE, FLIGHTDECK
AND CLASSIC SYSTEMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 4
GENERAL INSTALLATION INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 5
EXECUTIVE SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EXECUTIVE SYSTEM COMPONENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
EXECUTIVE STRUCTURAL MOUNTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
POST INSTALLATION TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRANSCEIVER INDICATIONS, PHONE SETTINGS AND OPERATIONS . . . . .
EXECUTIVE HANDSET REGISTRATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
RESETTING BASE STATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
HOW TO DIAL CALLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TROUBLESHOOTING TIPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OPERATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-1
4-1
4-1
4-5
4-5
4-6
4-6
4-6
4-7
4-7
4-9
4-9
FLIGHTDECK SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 - 1
Revision Date: March 24, 2007
i
Revision 5.0
FLIGHTDECK SYSTEM COMPONENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
FLIGHTDECK STRUCTURAL MOUNTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
FLIGHTDECK SYSTEM WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
POST INSTALLATION TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRANSCEIVER INDICATIONS AND PHONE SETTINGS . . . . . . . . . . . . . . . . . .
HOW TO DIAL CALLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TROUBLESHOOTING TIPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OPERATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5-1
5-1
5-1
5-2
5-2
5-2
5-3
5-3
CLASSIC SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CLASSIC SYSTEM COMPONENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CLASSIC STRUCTURAL MOUNTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CLASSIC WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
POST INSTALLATION TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRANSCEIVER INDICATIONS, PHONE SETTINGS AND OPERATIONS . . . . .
HOW TO DIAL CALLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TROUBLESHOOTING TIPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OPERATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6-1
6-1
6-1
6-2
6-2
6-2
6-2
6-3
6-3
TRACKER SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRACKER SYSTEM COMPONENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRACKER WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
POST INSTALLATION TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRACKER SETUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TRACKER TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7-1
7-1
7-4
7-5
7-5
7-5
7-7
TELEPHONE INDICATIONS and SETUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 - 1
TRANSCEIVER INDICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 - 1
PHONE TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 - 2
APPENDIX A Troubleshooting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 - 1
Revision Date: March 24, 2007
ii
Revision 5.0
LIST OF REVISIONS
Revision #
Description of Change
Date
Approval
2.0
Manual re-write
3/24/2005
MLF
2.01
Typo corrections and added info on A
model LBT
4/8/2005
MLF
2.02
Change on SOP Dialer dimming
4/25/05
MLF
2.1
Typo corrections and MMU additions
11/19/2005
MLF
2.2
Manual P/N change
12/13/2005
MLF
3.0
Consolidated POTS Systems, corrected 429
Conv. P.N., added description of 4.5 tracker
software, corrected pin out on FlightDeck
Drawing
4/17/2006
MLF
4.0
Reorganized the specifications into one
section. Reformatted paragraph numbers.
Added MMU and 11 position dialer notes.
11/13/2006
MLF
4.1
Corrected errors on Switch panel part
number and specs.
12/22/2006
MLF
4.2
Correction of 11 position dialer pinout and
description
1/18/2007
MLF
4.3
Addition of note in Section VII about data
charges
2/28/2007
MLF
5.0
Removed all legacy products
3/24/2007
MLF
Revision Date: March 24, 2007
iii
Revision 5.0
INDEX OF ACRONYMS
FOI
Field Of Interest (a position)
GIS
Geographic Information System
IDT
Icarus Dial Tone
IMEI
International Mobile Equipment Identifier
LBT
L Band Transceiver
PBX
Private Branch eXchange
POTS
Plain Old Telephone System
PUK
Personal Unblocking Code
SBD
Short Burst Data
SIM
Subscriber Identity Module
SMS
Short Message Service
For a complete definition of terms see http://www.telestial.com/glossary.htm on the Web.
Revision Date: March 24, 2007
iv
Revision 5.0
1
GENERAL INFORMATION
1.1
INTRODUCTION
This manual contains information relative to the physical, mechanical, and electrical
installation of the Sky Connect “Aviation” Systems. Operating procedures are also
included.
1.2
SYSTEM DESCRIPTION
The Sky Connect series satellite communications device consists of a transceiver, an
L-band antenna, and a dialing/audio/data interface device. The remote mounted
transceiver is the heart of the system, and contains the Iridium satellite LBT (L-Band
Transceiver). The LBT can be thought of as the “phone” in the satellite phone system and
the modem in the data system, as it is the connection used to gain access to the Iridium
network. The LBT allows the two way transfer of voice and data.
The LBT is the same in every transceiver of the Sky Connect System though different
modules are added to define the function of the transceiver as a whole. Phone versions
contain a POTS and/or DPL module allowing the LBT to be dialed and interfaced with
remotely. Each Sky Connect telephone system also has the ability for data transfer at
rates up to 10 Kbps (with compression), allowing the user to interface a laptop for
in-flight email capability, and in a pinch, website browsing. The Tracker system contains
an additional module and offers an optional internal 12 channel G.P.S. module. Tracker
uses the short burst data transfer portions of the Sky Connect suite, though it can be
coupled with any of the phone systems. Any system can exist alone, or co-exist with
another, and upgrades can be done to any system at any time without incurring additional
cost penalties.
The Iridium system can only be occupied by one “call” at a time, whether it is voice, data,
or Short Burst Data. These systems exist simultaneously, but can not be used
simultaneously. Multiple transceivers and antennas are required for multiple channels of
communication. For clarity, two users may be on separate handsets on the same call, but
two users can not be on separate handsets on different calls without a second
transceiver/antenna. Similarly, when a phone call is in progress, Tracker will be unable
to send SBD packets, though as soon as the line is clear, it will send its stored messages.
Revision Date: March 24, 2007
1-1
Revision 5.0
1.3
TECHNICAL SPECIFICATIONS
1.3.1
TRANSCEIVERS
Part Numbers 1616-XX0-0X all Transceivers are the same with the exceptions listed in
the below table.
ITEM
SPEC
Regulatory Compliance:
DO-160D, FAA STC on Part 25, 27, and 29 aircraft. FAA-PM A
Temperature Range:
Section 4 Cat D2 (-20C to +55C)
Altitude Range:
Section 4 Cat D2 (50,000 feet)
Vibration:
Section 8 Cat R
Temp Variation:
Section 5 Cat C
Power Input:
Section 16 Cat B
DC Spike:
Section 17 Cat B
Conducted Emissions
Section 21 Cat B
Radiated Emissions
Section 21 Cat B
W eight
4.05 lbs.
Add Tracker:
.05 lbs.
Add G.P.S.
.10 lbs
Add Messenger:
.05 lbs.
Physical Dimensions:
Length
10.0 Inches
(W idth)
2.5 Inches
(Height)
4.5 Inches
Power Requirements (Voltage):
11-32Vdc
Power Requirements (Current) :
<1 Amp @ 28Vdc
Transmit Power Average:
1.5 watts
Mounting:
Quick release tray, 4-#6 holes, any configuration
Transmission rate:
2.4Kbps voice and data (10Kbps with compression)
Operating Frequency:
1.616-1.6265 GHz
Revision Date: March 24, 2007
1-2
Revision 5.0
ITEM
SPEC
Inputs/Outputs:
POTS (Plain Old Telephone Service), RS232, DSC, dc
level. 8 discrete inputs Lo< 1.2 Hi >1.3
Connectors:
TNC female (Iridium), BNC female G.P.S.,
62 pin High Density D-sub connector
1.3.2
EXECUTIVE COMPONENT SPECIFICATIONS
1.3.2.1 Base Station
1616-101-01
ITEM
SPEC
Regulatory Compliance:
FAA STC on Part 25, aircraft.
W eight:
1.02 lbs.
Physical Dimensions:
Length
6.88 Inches
W idth
2.00 Inches
Height
4.56 Inches
Power Requirements (Voltage):
18-30Vdc
Power Requirements (Current) :
<0.1 Amp @ 28VDC
Operating Frequency:
2.4Ghz
Inputs/Outputs:
POTS (Plain Old Telephone Service)
Connectors:
9 pin Male Circular Amp, CPC
Mounting:
4-#6 holes through base station
1.3.2.2 CORDLESS HANDSET
1616-103-01
ITEM
SPEC
W eight:
.15 lbs. (phones .02 lbs. each considered carry on items)
Physical Dimensions:
Length
8.2 inches
W idth
3.43 inches
Depth
1.4 inches (1.25” below flush mount)
Revision Date: March 24, 2007
1-3
Revision 5.0
ITEM
SPEC
Power Requirements (Voltage):
11-32VDC
Power Requirements (Current) :
< .1 amp @ 28VDC
Connectors:
Screw terminals for input voltage
Mounting:
4- #6 tapped holes in cradle underside
1.3.3
FLIGHTDECK COMPONENTS SPECIFICATIONS (USING NAT PTA12 DIALPAD)
1.3.3.1 NAT PTA12-X00 DIALPAD
ITEM
SPEC
Regulatory Compliance:
DO-160D Env. Cat. A1/D1-BAB [(SBM)
(UF)]XXXXXXZBABB[UTX]MXXXX
Temperature Range:
-20 Celsius to +55 Celsius
Altitude Range:
50,000 feet
W eight:
.8 lbs.
Physical Dimensions:
(Depth)
4.17 Inches (behind panel including connector)
(W idth)
5.75 Inches
(Height)
1.12 Inches
Power Requirements (Voltage):
18-30VDC
Power Requirements (Current) :
.25 Amps @ 27.5VDC
Lighting Power Req (Current):
1 milliamp @ 27.5Vdc, .1 milliamp @ 5VDC
Inputs:
150 Ohm amplified Dynamic Mic. 250 mVrms
Mic Bias 13Vdc selectable on/off.
Outputs:
POTS (Plain Old Telephone Service)
Phones: 100mW into 600 or 150 Ohms
Connectors:
D-sub25 female
Mounting:
Dzus rail
Revision Date: March 24, 2007
1-4
Revision 5.0
1.3.4
CLASSIC COMPONENTS
1.3.4.1 HANDSET INTERFACE
1616-401-01/A
ITEM
SPEC
W eight:
6 Oz.
Physical Dimensions:
(Length)
1.75 Inches
(W idth)
3.50 Inches
(Height)
1.375 Inches
Inputs:
DSC, DC level
Outputs:
DC level
Connectors:
RJ45, D-sub 9
Interface Mounting:
4-#6 mounting holes
1.3.4.2 HANDSET and CRADLE
1616-403-01/A
ITEM
SPEC
W eight (Unit, Hardware):
.8 lbs
Cradle/Phone Physical Dimensions:
Length
8.5 Inches
W idth
2.0 Inches
Height
1.5 Inches (2.00 Inches with phone in cradle)
Cradle Mounting:
4- 4mm tapped holes
1.3.5.4 MISSION MANAGEMENT UNIT 1616-055-00
ITEM
SPEC
Regulatory Compliance:
FAA STC on Part 27, and 29 aircraft. FAA-PM A
W eight:
15 oz.
Physical Dimensions:
(Depth)
Revision Date: March 24, 2007
3.375 Inches
1-5
Revision 5.0
(W idth)
5.75 Inches
(Height)
1.875 Inches
Power Requirements (Voltage):
10-33 VDC
Power Requirements (Current) :
250 ma max.
Inputs:
RS-232
Outputs:
RS-232, four discrete outputs 100ma sinked to ground
Connectors:
DB-25 male
Mounting:
Dzus rail
1.3.5.7 CONFIGURATION/SIM MODULE 1616-905-02
ITEM
SPEC
Regulatory Compliance:
FAA STC on Part 27, and 29 aircraft. FAA-PM A
W eight:
16 oz.
Physical Dimensions:
(Length)
2.5 inches (without mating connectors)
(W idth)
2.125 inches
(Height)
.625 inches
Power Requirements (Voltage):
12VDC (supplied by transceiver)
Inputs:
Serial Buss and DPL Buss
Outputs:
Serial Buss and DPL Buss
Connectors:
One DE9 female and one DB25 male
1.3.6
ANTENNAS
1.3.6.1 IRIDIUM LOW PROFILE ANTENNA 1616-880-01 AeroAntenna AT2775-XXX
ITEM
SPEC
Regulatory Compliance:
TSO C-144, DO-160D
Operating Temp:
-55 Deg to +85 Deg C
W eight:
.5 Lbs Max.
Revision Date: March 24, 2007
1-6
Revision 5.0
ITEM
SPEC
Physical Dimensions:
3.5 inches in diameter
Frequency:
1595 +/- 30 Mhz
Connectors:
TNCF
Altitude:
70,000 feet
Impedance:
50 Ohms
1.3.6.3 SENSOR G.P.S. ANTENNA 1616-880-04
ITEM
SPEC
Regulatory Compliance:
TSO C-144, DO-160D
Operating Temp:
-67 Deg F to +185 Deg F
W eight
5 Oz.
Physical Dimensions:
3.5 inches in diameter X .57 Inches High
Frequency:
1575.42 MHz
Connectors:
TNCF
Altitude:
55,000 feet
Impedance:
50 Ohms
Voltage:
4 – 24 VDC
Revision Date: March 24, 2007
1-7
Revision 5.0
2
INSTALLATION PROCESS
INSTALLATION PROCESS OUTLINE
Note: Make a plan to cover the following items in depth in this manual.
2.1
WIRING DIAGRAM
2.1.1
2.1.2
2.1.2
2.1.3
2.1.4
2.1.5
Does this Phone have a tracker module installed? 1616-450 vs 1616400?
G.P.S. interface, or use of an internal G.P.S. -01 or -02?
Event switches, optional
Diagnostic port, must be installed for configuration
Configuration/SIM module, optional
Selection of Dialers optional
2.2
SIM CARD ACTIVATION
Check to make sure the card is activated, call Sky Connect
You will need to know the following information;
2.2.1
The form may be filled out on the web at http://www.skyconnect.aero/1086.xml
2.3
ANTENNA PLACEMENT PLAN
2.3.1
2.3.2
Pay close attention to the length of coax from the antenna to RT
Follow manual instructions on placement near other Sat COM and Comm antennas
2.4
IF Tracker Installed - INFORMATION NEEDED FOR CONFIGURATION
2.4.1
2.4.2
2.4.3
How the event switches were wired
What type of switches, MOM, ALT, Press
What phone numbers need to be entered (optional)
2.5
WIRING
2.5.1
Wire system as drawn, you the installer are responsible to the FAA for methods and
practices used during the installation.
Continuity checks.
Power polarity checks.
2.5.2
2.5.3
Revision Date: March 24, 2007
2-1
Revision 5.0
This page intentionally left blank
Revision Date: March 24, 2007
2-2
Revision 5.0
3
INSTALLATION - GENERAL
PRIOR TO INSTALLATION
Perform a visual inspection of the equipment for evidence of damage incurred during
shipment.
3.1
A DISCUSSION ON SIM CARDS
It is Sky Connect policy to ship all units with deactivated SIM cards. All units are
throughly tested with a DEMO card before leaving the factory. Your unit will work as
soon as the activation form is completed and return either by email or FAX to our office.
With that in mind, please be aware of the following paragraphs.
No testing can occur until a SIM card is activated in the transceiver or CONFIG/SIM
Module. The account has to be activated with an Iridium service provider. Systems are
generally shipped with a SIM card installed, with the PIN code disabled, and the service
deactivated. The customer is responsible for this activation as the customer receives the
bills for the phone use. This process can be done in munutes if the card is issued by Sky
Connect.
In the event that the customer provides a SIM card, or desires to provide the card it must
be de-pinned, or the system will get blocked. Contact the manufacturer if you intend to
change SIM cards. Sky Connect recommends against customer replacement of SIM cards
as it affects unit serviceability.
Until the Iridium L-Band Transceiver has been registered on the network, there is very
little you can do to test its operation. A de-pinned activated SIM is required before this
can happen. The SIM card is the identity of the user, and thus must travel with the user.
This process should only need to be accomplished at initial installation. After user
activation, the phone will function. Should the unit need to be replaced, or transferred to
another party, or in the event that a SIM card requires replacement, return unit to Sky
Connect or a qualified avionics shop to have the SIM card replaced in order to keep the
SIM card account matched with the user.
Revision Date: March 24, 2007
3-1
Revision 5.0
3.2
ITEMS REQUIRED BUT NOT SUPPLIED;
Table 1
QTY
ITEMS
USE
1
Daniels Manufacturing Crimper P/N M22520/2-01
P1
1
Daniels Manufacturing Crimper Positioner P/N K41
P1
1
Daniels Manufacturing Crimper Positioner P/N K1S
All M24308 connectors
Crimping tools for use on coax connectors
All coax connectors
Coax connectors for antenna cable if locally made
Contact insertion/removal tool
M81969/1-4 (metal) or
M81969/14-01 (plastic)
Misc. installations supplies such as; wire ties, Adel
clamps, Etc.
If installing a Tracker without the control head (ie
FlightDeck system with a Tracker) and panel mounted
switches are desired, we offer the following
manufacturer
part numbers with and without LEDs with and without
NVIS, non NVIS part numbers are not shown call
Vivisun
Vivisun# LED-40-18-KB-36190 (2JA CALL; 3JA
TEXT)
Call/Text - Annunciator
Vivisun# 95-40-18-K6-70957 (2JA CALL; 3JA TEXT)
Call/Text - Annunciator
Revision Date: March 24, 2007
3-2
Revision 5.0
3.3
Suggestions for coax connectors and tools (customer supplied);
Table 2
Connector
Coax
Tool
Newark#
Industrial#
BNC male
RG400/RG142
CTL-1
89F2891
31-4427
BNC male 90 Deg
RG400/RG142
CTL-1
39F1443
31-334
TNC female
RG400/RG142
220045-2
96F7801
225551-6
TNC female bulkhead
RG400/RG142
220045-2
97F8562
225557-6
TNC male
RG400/RG142
CTL-1
92B0647
31-4452
TNC male 90deg
RG400/RG142
220045-2
90B4658
225554-6
3.4
GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS
Table 3
Product
Part Number
Description
1616-700-01
Inmarsat Filter
1616-900-99
Sky Connect Series CD ROM
1616-950-XX
Aviation Installation Manual, current revision
1616-901-XX
Quick Start User Manual, current revision
1616-050-80
SBD Message Traffic
1616-104-01
3 year warranty
S67-1575-109
Low Profile Iridium Antenna
1616-429-01
ARINC 429 Converter for converting to RS232
1616-105-02
RT Installation kit which consist of:
1.) 1616-720-07 DD62F00000 – Positronics connector
2.) 1616-721-01 FC8022D - Positronics contacts
3.) 1616-722-06 D37000Z00 – Positronics hood
Revision Date: March 24, 2007
3-3
Revision 5.0
3.5
SYSTEM COMPONENTS THAT APPLY ONLY TO EXECUTIVE, FLIGHTDECK
AND CLASSIC SYSTEMS
Table 4
Description And
Part Number
Components
Product
Executive
FlightDeck
Classic
1616-400-01A
RT for phone use only
1616-450-01A
RT for phone use with internal
Tracker and internal G.P.S.
1616-450-02A
RT for phone use with Tracker
and no G.P.S.
1616-880-01
Iridium Antenna AT2775-110GAW-TNCF
1616-880-04
G.P.S. antenna S67-1575-39
1616-900-01
Installation Kit consist of; tray, Iridium antenna,
connector kit, G.P.S. antenna and Install CD
1616-900-02
Same as above but without G.P.S. antenna
1616-105-01
Transceiver tray
1616-150-01U
Upgrade kit for adding Tracker with G.P.S. to POTS
system
1616-150-02U
Upgrade kit for adding Tracker without G.P.S. to
POTS system
The above RTs apply to all Full Telephony systems.
See Section VII for a list of Tracker/Tracker w/Voice Components
The following table is a list of older part numbers and their newer replacement numbers.
Older Part Numbers
Newer Replacement Numbers
1616-100-01/A, 1616-300-01/A
1616-400-01A
1616-150-01/A, 1616-350-01/A
1616-450-01A
1616-150-02/A, 1616-350-02/A
1616-450-02A
The above change in numbers was to allow the already FAA STCd, PMAd part numbers to be
used as replacement for older systems.
Revision Date: March 24, 2007
3-4
Revision 5.0
3.6
GENERAL INSTALLATION INSTRUCTIONS
3.6.1
ANTENNA PLACEMENT
The Aero-Antenna AT2775 L-Band antenna should be placed as far as practical from
other transmitting antennae. A minimum of 30 inches is recommended to other L-Band
transmitting antennae. The Iridium antenna is itself a transmitting antenna, and as such,
an eighteen inch minimum spacing to G.P.S. antennae is recommended. The Iridium
antenna requires full view of the sky above. Shadowing and interference can occur when
mounted near vertical stabilizers, and other structures inherent to aircraft. When used in
conjunction with an internal G.P.S. for Tracker, a separate active Sensor S67-1575-39
G.P.S. antenna is supplied. See Figure 4 for antenna dimensions.
Note: Inmarsat systems (commonly referred to as Satcom) will greatly interfere
with the performance of the Iridium antenna. This interference may appear to be
intermittent with aircraft position as the Inmarsat transmitting antenna array is
electrically steer able depending on azimuth to satellite. Inmarsat will disrupt
Iridium communications whenever active. Inmarsat should be disabled when
Iridium is in use, alternatively, filters are available for Inmarsat systems which
essentially act as an Iridium bandpass filter. Consult Sky Connect for more
information.
The antenna should be mounted in accordance with the manufacturer’s instructions and
reference FAA AC43.13-2A. The antenna should be properly bonded to the aircraft
ground plane to aid in eliminating unwanted interference. Surface preparation should
include the use of Alodine 1001 or similar. The antennae listed above, as well as the
Sensor S67-1575-109 Iridium antenna are all TSO’d and approved for mounting on
pressurized vessels.
Antenna installations on pressurized vessels require FAA approved design and
engineering data whenever a pressure vessel requires penetration due to
connector/mounting holes. Approved designs can be obtained from aircraft
manufacturers, STC data specific to the antenna, or DERs. Seal antenna in accordance
with FAA AC43.13-2A.
Revision Date: March 24, 2007
3-5
Revision 5.0
3.6.2
ANTENNA CABLE
When routing antenna cable, avoid high current wiring, other transmitting antenna cables,
and sharp bends. Antenna cable should be selected to obtain 3dB max loss at 1.6GHz.
The installer is responsible for providing antenna cables. Use the following chart as an
aid to determine the appropriate cable type for your required installed length. Follow
industry practices when assembling the TNC connectors. RG-142 coax cable is
recommended in installations up to 20 feet in length, alternative cable types are listed
below.
Pre assembled cable lengths are available from EMTEQ, ECS, and PIC.
Table 5
Cable Length
EMTEQ
ECS
PIC
< 15 feet
PFLX195-100
352001
S33141
15-25 feet
PFLX240-100
311601
S33141
25-40 feet
PFLX340-100
311201
S55122
310801
S22089
35-60 feet
3.6.3
TRANSCEIVER STRUCTURAL MOUNTING
The Sky Connect Transceiver should be mounted in accordance with standard practices
found in FAA Advisory Circular 43.13-2A. The Transceiver is approved for mounting
outside the pressure vessel. See Figures 2 and 3 for unit and tray dimensions.
The structural mount consists of a mating tray, with a self-locking, vibration resistant,
knurled thumbscrew system. The tray should be bolted to a suitable avionics shelf, using
approved #6 hardware. The 62 pin High Density D-subminiature connector and 1 to 2
antenna connectors are all that is required to electrically connect the box once it has been
structurally secured in place.
3.6.4
TRANSCEIVER ELECTRICAL INSTALLATION
Wiring must be done in accordance with FAA AC43.13-1B, or most current revision. A
Revision Date: March 24, 2007
3-6
Revision 5.0
crimp tool meeting Mil Spec M22520/2-01 and a positioner are required to ensure
consistent, reliable crimp contact connections for the 62-pin D Subminiature connector.
A 2 amp pull able Circuit Breaker is required for external protection of the Sky Connect
Transceiver. All wiring is 18-22AWG, and should use Mil Spec 22759/16 or 27500/18
wire or wire deemed appropriate to the aircraft type by the governing aviation regulatory
agency. See the appropriate following Sections for the schematics of your system for
wiring examples.
See Table 1 above for recommendations of discreet switches to be installed when not
installing a Sky Connect control head with internal switches.
Note: Sky Connect telephony systems are generally considered non-essential and
should be treated as such when selecting the appropriate bus for power. The system
should be placed behind a nonessential bus. However if the mission of the aircraft
deems the Sky Connect System safety sensitive, the essential buss may be used. An
electrical load analysis may be required when doing so.
Revision Date: March 24, 2007
3-7
Revision 5.0
3.6.5
TRANSCEIVER PIN ASSIGNMENTS
The below Table is a listing of pin assignments and signal flows. Read Notes and pay
attention to the asterisk for changes in Original and “A” Model. DSC was the Classic
original buss, DPL is used on all A model units.
Table 6
* denotes changes in A Model SOP units and others with newer version of LBT
Pin
Description
Flow
15
Annunciator #1 –Sinks 100ma to
Ground
Out
1
Ground Input
Gnd
2
Ringer output or Audio Enable Input.
SEE NOTE 1
In/Out
16
Annunciator #2 – Sinks 100ma to
Ground
Out
2*
A Model only PCM Transmit or IDT
ground IMPORTANT - DO NOT
STRAP AS AUDIO ENABLE ON SOP
A MODEL
Gnd
17
Annunciator #3 – Sinks 100ma to
Ground
Out
18
Annunciator #4 – Sinks 100ma to
Ground
Out
3
Comm Audio Lo or POTS audio shield
Gnd
19
Configure SDA--Do Not Connect to
other than Sky Connect Configuration
Module
4
DSC/DPL Uplink (Classic Systems
only)
In
5
PC DCD (Data Connections only)
Out
20
Event switch #1 – Gnd=Active
In
6
NC
21
11-33VDC positive voltage input
In
6*
IDT DPL Mic audio Hi
In
22
Ground Input
Gnd
7
Microphone Audio Hi/POTS Ring. SEE
NOTE 2
In
23
DSC Gnd (Classic Systems only)
Gnd
23*
DPL Ground (Classic Systems only)
SOP A – PCM receive
Gnd/In
7*
Mic Audio Input for SOP A Model
In
8
Program Stat --Factory Use Do Not
Connect
24
Program -TX-- Factory Use Do Not
Connect
9
Shield/Configure ground
Gnd
25
DSC/DPL Downlink (Classic Systems
only)
Out
10
Shield/Configure ground
Gnd
26
DSC Enable (Classic Systems only)
Out
11
Shield/Configure ground
Gnd
26*
Out
Configuration Module Power
(3.3V)--Do Not Connect to other
than ICM
Out
DPL Enable (Classic Systems only)
SOP A – PCM Frame Sync
12
27
PC CTS (Data Connections only)
Out
28
Configure SCL
In
13
Shield/Configure ground
Gnd
29
Shield/Configuration ground
Gnd
Com Audio Hi/POTS Tip. SEE NOTE
3
Out
14
29*
Com Audio Hi
Out
Revision Date: March 24, 2007
3-8
Revision 5.0
Pin
Description
Flow
30
Diagnostics Gnd
Gnd
31
RS232 #1 Gnd
Gnd
32
RS232 #2 Gnd
Gnd
33
Shield/Configure ground
Gnd
34
Program Md0--Factory Use Do Not
Connect
54
Program-RST-- Factory Use Do Not
Connect
55
Event switch #8 – Gnd=Active,
configuration. switch style
(mom,alt,dial,sqt)
In
56
Event switch #7 – same as pin 55
In
57
Event switch #6 – same as pin 55
In
35
Shield/Configure ground
Gnd
58
Event switch #5 – same as pin 55
In
36
PC GND (Data Connections only)
Gnd
59
Event switch #4 – same as pin 55
In
37
PC S TX (Data Connections only)
Out
60
Event switch #3 – same as pin 55
In
38
PC DTR (Data Connections only)
In
61
Event switch #2 – same as pin 55
In
39
PC RTS (Data Connections only)
In
62
11-33VDC positive voltage input
In
40
Program Rx--Factory Use Do Not
Connect
Note
1
Out
41
Ringer Hi (Input Voltage)
Out
Executive, Classic and FlightDeck
systems=Ringer Lo-Gnd
Output to drive Piezio alert or light
(100mA).
42
11-33VDC positive voltage input
In
In
43
Ground Input
Gnd
44
NC
Tracker SOP systems=Configuration
strap for Audio Enable
Tracker SOP A Model DO NOT USE
AUDIO ENABLE!
44*
PCM clock (Classic System only) SOP
A IDT DPL Audio Out
Out
Executive, Classic and FlightDeck
systems=POTS Ring (or Tip)
In/Out
45
PC RI (Data Connections only)
Out
Tracker SOP systems=Mic Audio In
In
46
PC DSR (Data Connections only)
Out
Tracker SOP A does not allow full
Telephony
47
Data out Hi – Diagnostics output
Out
48
RS232 #2 Hi – Messenger output
Out
49
Data in Hi – Diagnostics input
In
50
RS232 #2 Hi – Messenger input
In
51
PC S RX (Data Connections only)
In
52
RS232 #1 Hi – Serial G.P.S. input
In
53
Program-md1-- Factory Use Do Not
Connect
Revision Date: March 24, 2007
Note
2
Note
3
3-9
Executive, Classic and FlightDeck
systems=POTS Tip (or Ring)
In/Out
Tracker SOP systems=Comm Audio
Out
Out
Revision 5.0
Figure 2
View of connector from rear (side contacts insert in)
Figure 3
Sky Connect Transceiver Dimensions
Revision Date: March 24, 2007
3 - 10
Revision 5.0
Figure 4
Transceiver Installation Clearances
Revision Date: March 24, 2007
3 - 11
Revision 5.0
Figure 6
Dimensions of the Sensor Systems GPS Antenna
Revision Date: March 24, 2007
3 - 12
Revision 5.0
Revision Date: March 24, 2007
3 - 13
Revision 5.0
Figure 7
Dimensions for the Sensor Systems GPS Antenna
Revision Date: March 24, 2007
3 - 14
Revision 5.0
4
EXECUTIVE SYSTEM
4.1
INSTALLATION
Be sure to cover Section III as it pertains to the transceiver installation and antenna
installation that applies to all systems.
All systems are capable of having the Tracker options installed. For Tracker installation
and system testing and operation see Section 7.
4.2
EXECUTIVE SYSTEM COMPONENTS
Table 7
Description
And Part Number
Components
Product
Executive
1616-100
See Section III
for RT and
related part
numbers
1616-101-01
Base Station, with connector
1616-200-01
Surface Mount, painted
Black, with handset
1616-200-01-X
Surface Mount, unpainted,
with handset
1616-200-02
Flush Mount, painted Beige,
with handset
1616-200-02-X
Flush Mount, unpainted, with
handset
1616-295-xx
Cradle w/o power supply
1616-295-xx
Cradle back plate only
1616-297-01
Cradle power supply
1616-103-01
replacement handset
1616-102-02
AC powered battery charger
for spare batteries
1616-102-03
AC powered phone charger
Revision Date: March 24, 2007
4-1
Revision 5.0
Figure 8
Cradle Charger Wiring
Revision Date: March 24, 2007
4-2
Revision 5.0
Figure 9
Cradle Dimensions
Revision Date: March 24, 2007
4-3
Revision 5.0
Figure 9.1
Cordless Phone Base Station
1616-101-01
Revision Date: March 24, 2007
4-4
Revision 5.0
4.3
EXECUTIVE STRUCTURAL MOUNTING
The Sky Connect Executive components should be mounted in accordance with standard
practices found in FAA Advisory Circular 43.13-2A.
The remote phone cradles are designed for flush mounting either horizontally or
vertically as they have a positive locking detent. There are four tapped #6 holes
on the underside of the cradle to allow specific mounts to be tailored to the
aircraft. Surface mount cradles are identical in mounting to the flush cradles, but
lack the flanged edge. They are designed for use in drink rails, on partitions, or
armrests. They also may mount horizontally or vertically.
The base station must be located within the aircraft cabin, and outside of complete
aluminum enclosures. The base station should be bolted to a suitable shelf, panel,
floor board, or cabinet, using approved #6 hardware. When choosing a location
for the base station, allow access to the small white reset button located on one of
the large faces. This white button is used for programming and resetting the base
station to the handsets. The 9 pin circular connector is all that is required to
electrically connect the base station once it has been structurally secured in place.
4.4
WIRING
4.4.1
CRADLE WIRING
Executive charging cradles each require power to be supplied and may utilize the
same breaker as the base station, but should be individually fused at the cradle to
no more than ½ amp. Follow the illustrations in drawing to connect the cradles.
Remove the two screws from the small cover below the charging mount. Route
11-32 VDC through hole in cradle underside to “V+/V- In” screw terminals.
Mechanically secure wires in terminals then provide internal strain relief for the
cable. Close the access cover and secure.
4.4.2
TRANSCEIVER WIRING
Refer to SECTION III
Revision Date: March 24, 2007
4-5
Revision 5.0
4.4.3
EXECUTIVE SYSTEM WIRING
Follow the installation drawing 1616-900-100 for the interconnection of the
Executive system into the aircraft. As always pay close attention to the notes that
apply to that drawing. The Executive Base station requires a 1 amp pull able
Circuit Breaker for external protection.
4.5
POST INSTALLATION TESTING
No testing can occur until a valid SIM card is installed in a transceiver, the PIN code
turned off, and the account has been activated with an Iridium service provider. Systems
are generally shipped with a SIM card installed, with the PIN code disabled, and the
service inactive. The customer is responsible for this activation as the customer receives
the bills for the phone use. This process can take a day, and should be done in advance of
the installation/testing.
4.6
TRANSCEIVER INDICATIONS, PHONE SETTINGS AND OPERATIONS
Refer to Section VIII for a description of how;
4.6.1
4.6.2
The transceiver indicates during normal operation.
To test the phone.
4.7
EXECUTIVE HANDSET REGISTRATION
In order to use your Siemens 4200 handsets, you must first register all handsets to the
base station in the aircraft. If you are registering a new set of phones to the base
station and want to de-register an old set of phones, please go first to the Reset
instructions below. Executive systems are shipped with handsets that are not
necessarily assigned to the base station, so this task should be accomplished in the
field prior to the testing and use of the Executive System. A handset that a remains
“Searching” for an excessive time is either not registered, or this is an indication that
the base station is not powered.
4.7.1
4.7.2
4.7.3
4.7.4
Be sure that the base station and the Sky Connect Transceiver are powered up.
Power the phone by holding the RED button down until the unit turns on.
Note: Whenever “OK” is required, press the soft key under “OK”.
Press MENU.
Go to H/Set Settings using the round rocker switch, press OK.
Revision Date: March 24, 2007
4-6
Revision 5.0
4.7.5
4.7.6
4.7.7
Go to Reg Handset, OK.
Select Base 1, OK.
All handsets must be registered to Base 1. Each handset will be issued its own
intercom position, 1-4.
4.7.8 Enter a PIN of “0000”, OK.
4.7.9 Hold down the small button on the base station until the phone responds
with flashing and noises. This button is only 1/8" in diameter, and is on the RHS of the
base station when looking at the connector end of the unit.
4.7.10 Repeat for the 2nd phone. One will display INT1 and the other INT2.
4.7.11 Repeat as necessary for phones 3 and 4.
4.8
RESETTING BASE STATION
Resetting the base station un-registers all handsets previously registered to that base
station. Prior to power up, hold down the reset button on the base station. This button is
only 1/8" in diameter, and is on the RHS of the base station when looking at the
connector end of the unit.
Apply power and continue to hold down the reset button for 10 seconds. Confirm
handsets are un-registered by looking at handset display where “searching” should be
displayed.
You will have to use the above procedure to re-register all handsets that need to
access that base station.
4.9
HOW TO DIAL CALLS (REF. CIL 2006-002 ON WEBSITE www.skyconnect.aero)
Press the green key to get a dial tone.
Note: If you do not have a dial tone at this point, and hear 3 repeating melodic
tones are heard, do not dial. Your SIM card is not de-pinned. Consult technical
support.
Dial the country code, area code, and number followed by the pound key. The pound
key is required to alert the phone that the end of the dial string has been reached. No
call will be initiated without the pound key. You will hear call progress tones
followed by the ringing sound. For calls within the US, for example, dial as follows:
Revision Date: March 24, 2007
4-7
Revision 5.0
001-301-891-0600-#, where “00” is international access, “1” is the country code for the
US, and “#” is the end of the dialing string. You may also pre-dial before getting a dial
tone by simply keying in the number, then hit the green key to “send” the call as you
would on a cell phone. Optionally, dialing strings can be stored in phone memory
locations.
The phone may be completely shut off by holding down the red key. This will save
the rechargeable batteries from discharging. Holding this same red key down will
also turn the phone on.
Note: The rechargeable batteries in the phone become a part of the circuit when
the handset is placed in the cradle. DO NOT USE ALKALINE OR
OTHERWISE NON-RECHARGEABLE BATTERIES. Placing nonrechargeable batteries in a charger is dangerous. Do not store handsets without
batteries in the charger.
Note: Turning power on to the aircraft (or buss powering the base
station) will cause the handsets to turn on. Turning off the power to
the base station WILL NOT turn off power to the handsets. Handsets
must be powered down individually. It is recommended that the
handsets be powered down and stowed in on board storage other than
the cradles as a function of the pilot’s power-down checklist. Press
and hold the red “End” key until the handset powers down. This will
avoid inadvertent powering and discharging of the handsets, and
alleviate the concern of handset misplacement or theft.
Revision Date: March 24, 2007
4-8
Revision 5.0
4.10
TROUBLESHOOTING TIPS
Refer to Appendix A for troubleshooting advice or the following chart for handset to base
station help.
Fault
Possible Causes
Possible Solution
No display
Handset not activated
Batteries dead
Hold down end call key for 1
second
Charge or replace batteries
No reaction to key stroke
Keypad protection activated
Hold down the “#” key for 1
second
No radio connection to the
base station – ei base
station 1 flashing
Handset outside base station
range
Handset not registered
Base station not powered
Move closer to base
Handset does not ring
Ringer off
Hold down the “*” key
You can not hear
Microphone is muted
Press the “Escape” key
Error beep is generated
(descending tone sequence)
Wrong input
Repeat the procedure; note
the display
4.11
Register the handset
Check to make sure the base
station connector has 1830VDC
OPERATIONS
The Sky Connect Executive system consists of the Sky Connect Transceiver and L-band
antenna, as well as a wireless base station, up to four wireless handsets, and flush or
surface mounted charging cradles.
The wireless base station is mounted within the aircraft cabin and is the aircraft
equivalent to the base station you would find in any wireless phone system for home use.
The Siemens 2.4GHz wireless handsets are fully functional phones that dial the Sky
Connect Transceiver via the base station interface. In addition to all of the functions you
would find in a normal wireless handset, multiple intercom and speaker phone functions
are available allowing a great deal of flexibility in party line conferencing, as well as
cabin communications. The handsets will work up to 300 feet from the aircraft while on
the ground, though this is not recommended in flight.
Revision Date: March 24, 2007
4-9
Revision 5.0
5
FLIGHTDECK SYSTEM
INSTALLATION
Be sure to cover Section III as it pertains to the transceiver installation and antenna
installation that applies to all systems.
All systems are capable of having the Tracker options installed. For Tracker installation
and system testing and operation see Section VII.
5.1
FLIGHTDECK SYSTEM COMPONENTS
Table 8
5.2
Description
And Part Number
Components
Product
FlightDeck
1616-300
See Section III for
RT and related part
numbers
1616-301-01
NAT PTA Dialing controller
with Connector
FLIGHTDECK STRUCTURAL MOUNTING
The Sky Connect FlightDeck should be mounted in accordance with standard
practices found in FAA Advisory Circular 43.13-2A. The FlightDeck dial pad is the
NAT PTA12. This is a Dzus mounted unit and will mount in any standard Dzus rail.
Adapters are available to convert Dzus for use in a standard 6.25” tray. For specific
mounting information, refer to the NAT PTA12 Installation Manual. For specific
audio interfaces, refer to appropriate installation manual, or contact Sky Connect
Instruments Tech Support for assistance.
5.3
FLIGHTDECK SYSTEM WIRING
Follow the installation drawing 1616-912-XX for the interconnection of the
FlightDeck system into the aircraft. As always pay close attention to the notes that
apply to that drawing. For complete wiring instructions of the Northern Airborne
Revision Date: March 24, 2007
5-1
Revision 5.0
Technology PTA12, see the current revision of that manual from NAT.
5.4
POST INSTALLATION TESTING
No testing can occur until a valid SIM card is installed in a transceiver, the PIN code
turned off, and the account has been activated with an Iridium service provider. Systems
are generally shipped with a SIM card installed, with the PIN code disabled, and the
service inactive. The customer is responsible for this activation as the customer receives
the bills for the phone use. This process can take a day, and should be done in advance of
the installation/testing.
5.5
TRANSCEIVER INDICATIONS AND PHONE SETTINGS
Refer to Section VIII for a description of how;
5.5.1
5.5.2
The transceiver indicates during normal operation.
To test the phone
5.6
HOW TO DIAL CALLS (REF. CIL 2006-002 ON WEBSITE www.skyconnect.aero)
5.6.1
Press the “Hook” key to get a dial tone.
Note: If you do not have a dial tone at this point, and hear 3 repeating
melodic tones are heard, do not dial. Your SIM card is not de-pinned.
See Appendix A for troubleshooting advice.
5.6.2
Dial the country code, area code, and number followed by the pound key. The pound key
is required to alert the phone that the end of the dial string has been reached. No call will
be initiated without the pound key. You will hear call progress tones followed by the
ringing sound. For calls within the US, for example, dial as follows:
001-301-891-0600-#, where “00” is international access
“1” is the country code for the US, and
“#” is the end of the dialing string.
For complete instructions on how to use the PTA12, see the Northern Airborne
Technology Manual.
Revision Date: March 24, 2007
5-2
Revision 5.0
5.7
TROUBLESHOOTING TIPS
Refer to Appendix A for troubleshooting advice.
5.8
OPERATIONS
The Sky Connect FlightDeck system consists of the Sky Connect Transceiver and L-band
antenna, as well as a Dzus rail mounted dial pad/audio interface. This system is designed
for use in the cockpit, utilizing the aircrafts headsets as the audio interface. When used in
combination with Executive, party line functionality is obtained. Cabin communications
and conferencing are available via the dial pad/audio interface when used in conjunction
with a PBX. The dial pad is used for the dialing and answering of calls. Once connected
to a call, the flight crew is capable of communicating in a full-duplex fashion directly
through their headsets.
Sky Connect manufactures a number of Sat Com/Headset audio interfaces to allow more
flexibility depending on the specific aircrafts needs.
Revision Date: March 24, 2007
5-3
Revision 5.0
6
CLASSIC SYSTEM
INSTALLATION
Be sure to cover Section III as it pertains to the transceiver installation and antenna
installation that applies to all systems.
All systems are capable of having the Tracker options installed. For Tracker installation
and system testing and operation see Section VII.
6.1
CLASSIC SYSTEM COMPONENTS
Table 9
6.2
Description
And Part Number
Components
Product
Classic
1616-400
See Section III for
RT and related
part numbers
1616-401-01/01A
Handset Interface
1616-402-01/02
Hang-up Cup
1616-403-01/02
Handset
1616-405-01/02
Handset kit
CLASSIC STRUCTURAL MOUNTING
The Sky Connect Classic should be mounted in accordance with standard practices
found in FAA Advisory Circular 43.13-2A. To mount the Classic Handset Cradle,
install 4- 4mm screws into the rear of the cradle. Mount the cradle to any suitable
armrest, interior panel, drawer, divider, or other structural member. The cradle can
mount horizontally or vertically and has a locking detent. Mount the handset
interface box in a suitable location near the handset, as the handset plugs directly in to
the interface using an RJ-45 connector. The ringing PIEZIO alert for the handset is
contained within the interface box. A trim pot on the interface allows selection of
alert volume. Four #6 holes are provided for Classic interface mounting. If the
interface is mounted behind interior an auditory test should be done with engines
running to ensure adequate alert volume. Handset cable should feed through a hole in
the interior located behind the mounting cradle for cleanest aesthetics.
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Note: The Classic Handset and cradle are considered small parts in
accordance with FAR 25, Appendix F, Part 1, Paragraph (a).(1).(v)
when used in a single handset configuration, and therefore meet the
flammability requirements of FAR 25.853. Multiple installations of
handsets will not meet the flammability requirements of FAR 25.853.
The handset cord meets or
exceeds the electrical wiring flammability requirements of FAR 25,
Appendix F, Part 1, Paragraph (a).(3).
6.3
CLASSIC WIRING
Follow the installation drawing 1616-914-01 for the interconnection of the Classic
system into the aircraft. Use drawing 1616-914-02 for the Classic A system, as the
interface to the handset has changed for that system. As always pay close attention to
the notes that apply to that drawing. Classic handsets interface via an external
interface box using a 9 pin D-subminiature connector and the handsets RJ-45
connector. A maximum of 30’ between transceiver and the Classic handset is
allowed. RG-316 or equivalent wiring must be used for the DSC bus data signals.
Maximum overall length of DSC buss is 30 feet including compressed coil cord. The
DPL buss is not limited.
6.4
POST INSTALLATION TESTING
No testing can occur until a valid SIM card is installed in a transceiver, the PIN code
turned off, and the account has been activated with an Iridium service provider. Systems
are generally shipped with a SIM card installed, with the PIN code disabled, and the
service inactive. The customer is responsible for this activation as the customer receives
the bills for the phone use. This process can take a day, and should be done in advance of
the installation/testing.
6.5
TRANSCEIVER INDICATIONS, PHONE SETTINGS AND OPERATIONS
Refer to Section VIII for a description of how;
6.5.1
6.5.2
The transceiver indicates during normal operation.
To test the phone
6.6
HOW TO DIAL CALLS (REF. CIL 2006-002 ON WEBSITE www.skyconnect.aero)
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Dial “00,” the country code, area code, and number followed by the “OK” key. The
“OK” key is required to alert the phone that the end of the dial string has been
reached. No call will be initiated without the “OK” key. You will hear call progress
tones followed by the ringing sound. For calls within the US, for example, dial as
follows: 001-301-891-0600-OK, where “00” is international access, and the “1” is the
country code for the US. Optionally, dialing strings can be stored in phone memory
locations.
The Classic handset should not be unplugged while the system is on. If necessary to
unplug the handset, or if the handset was unplugged inadvertently, the system must be
powered down and the handset reconnected before power is applied. No damage will
be done to the handset, though the system may not operate correctly until restart.
6.7
TROUBLESHOOTING TIPS
Refer to Appendix A for troubleshooting advice.
6.8
OPERATIONS
The Sky Connect Classic system consists of the transceiver and L-band antenna, and uses
a corded handset for dialing/communicating. The Classic configuration contains limited
memory dialing functions. When used in conjunction with FlightDeck, access to the
transceiver is on a first come, first serve basis. Ringing audio is provided through a small
PIEZIO alert which is housed in the Classic handset interface. Volume of the alert is
selectable via a trim pot adjustment. A “Ground” output is available at the interface for
additional external annunciator/alerts. A maximum of thirty feet from Transceiver to
handset is permitted on the DSC buss. This measurement includes path to handset as
well as the collapsed coil length. This length restriction does not apply to the new
Iridium DPL handset.
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7
TRACKER SYSTEM
INSTALLATION
Be sure to cover Section III as it pertains to the transceiver installation and antenna
installation that applies to all systems.
NOTE:
7.1
All added features to the Tracker, such as Altitude Trigger, and
Change of Flight Plan feature can increase the cost of operation of the
tracker. Check with your operations department prior to turning on
features that may increase the cost of operation. Once the data is sent
over the system, there will be a charge for the use of the data.
TRACKER SYSTEM COMPONENTS
Table 10
Description
And Part Number
Components
Product
S67-1575-39
G.P.S. Antenna 1616-050-01/03/05 only
1616-055-00
MMU (Mission Management Unit)
1616-905-01
Configuration Module
1616-905-02
Configuration/SIM Module
1616-105-01
Transceiver Mounting Tray
1616-050-99
Tracker Setup CD ROM
1616-900-01
Tracker w/G.P.S. install kit contains;
Tray, Connectors, Iridium antenna, G.P.S.
antenna, Manuals, Software
1616-900-02
Tracker no G.P.S. install kit contains;
Tray, Connectors, Iridium antenna, Manuals,
Software
1616-900-03
Tracker SOP w/G.P.S. install kit contains;
Tray, Connectors, Iridium antenna, G.P.S.
antenna, Manuals, Software
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Description
And Part Number
Components
Product
1616-900-04
Tracker SOP no G.P.S. install kit contains;
Tray, Connectors, Iridium antenna, G.P.S.
antenna, Manuals, Software
(Not to scale)
Figure 11
Mission Management Unit (MMU)
11 position SOP Dialer
7.1.2
CONFIGURATION MODULE
The Configuration Module (ICM) part number 1616-905-01, if used should be
installed within 8” to the 62 pin connector and secured to the harness. The
configuration module stores settings external to the transceiver and also provides
a female connector for easy connection to a PC via straight PC cable for system
configuration. The purpose of the module is to alleviate the need to reprogram to
an individual aircraft if units are shifted amongst the fleet. Removal and
replacement of the Sky Connect Transceiver with a different unit will keep the
Users stored settings the same, though a tail number to serial number
configuration mismatch will be logged as a security procedure via the iridium
network. Theft for re-use of the Sky Connect Tracker is impractical, as not only
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do we know who you are, but exactly where you are! Regardless, the
configuration procedure only needs to occur once, or when a configuration
module is replaced. An additional use for the configuration module would be to
update all of the phone numbers in a fleets system. This becomes a time saving
device allowing one module to program each aircraft, only necessitating the
update of the individual tail numbers.
The male connector on the ICM connects via 6 wires to the 62 pin connector of
the Tracker system. The female connector is the configuration port for both the
ICM and the Tracker itself. If the configuration module is in place during
programming, settings are saved to the transceiver and to the ICM. If the ICM is
connected at startup, the configuration is read from the ICM. If it is not present at
startup, the system uses its internal memory which is re-flashed by the ICM at
startup when connected.
7.1.3
CONFIGURATION/SIM MODULE
The Configuration/SIM Module (ICSM) part number 1616-905-02, has the same
functionality as the Configuration Module but allows for the installation of the
SIM card into the module instead of the transceiver. With this setup no card need
be installed in the transceiver at all. This allows for the swapping of the unit, and
the SIM card to remain with the aircraft. No changes to the aircraft’s phone
number. A secondary advantage would be if the customer changed voice
providers, the ICSM could be opened and the card installed, eliminating
maintenance to the transceiver itself.
NOTE: While the female connector on the ICM/ICSM is
designed to be connected directly to a PC for programming, the
PC should not be connected directly to the installer provided
female connector used to connect to the ICM’s male connector.
Only pins 2, 3, and 5 are used for configuration, the remainder
of the pins are used internally and damage can be done to the
Tracker and the PC if these lines are connected to a PC
inadvertently. See wiring diagrams.
7.1.5
MMU (Mission Management Unit)
This unit is a computer controlled dialer and is very flexible in
operation. It speaks to the transceiver over an RS-232 port. This unit
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can be programmed in the aircraft with new message sets, or software.
It has a four step dimming feature to the display.
7.3
TRACKER WIRING
Follow the installation drawing 1616-910-XX for the interconnection of the Tracker
system into the aircraft. As always pay close attention to the notes that apply to that
drawing. Wiring of the Tracker system is mission specific. Tracker can be entirely
standalone, or tied to multiple aircraft systems. The Tracker system is designed to be
extremely flexible with open architecture. Switched input options are limited only by the
customer and the specific capabilities of the GIS software used for aircraft tracking.
The MMU lighting is controlled from the lighting buss, but the unit does not draw
current from the buss. The control is used to “follow” the dimmer buss voltage and
when this voltage gets within 20% of the low end of the scale, the unit will illuminate
to full brightness for day light use. This is designed for aircraft that loose dimmer
voltage when the dimmer is turned off.
See paragraph below, for installations that use a MMU and a GPS that does not supply
altitude data, the serializer may be input through the diagnostics port. This should be
done using the 9 pin connector as on the drawings, so the serializer may be disconnected
when time to connect a PC.
When using an external GPS receiver, in order for the Tracker to include aircraft altitude
in the data that is sent to the ground, a Garmin GPS receiver (430/530/480, etc) must be
used in order to get altitude data from the navigation RS-232 data stream.
For GPS receivers such as the KLN-90B, KLN-900, etc which DO NOT supply altitude
in their serial stream, a source of serial altitude data in the Icarus (Garmin) format at
9,600 baud must be supplied to the Tracker. There are multiple sources available for
serial altitude data in this format including certain Garmin transponders, encoders with a
serial output, and the Icarus 3000U serializer. Please consult technical support for further
details.
For aircraft not equipped with a navigation source that outputs RS-232, Sky connect
builds a ARINC429 to RS-232 converter that will handle the input of GPS data to our
trackers.
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7.4
POST INSTALLATION TESTING
No testing can occur until a valid SIM card is installed in a transceiver, the PIN code
turned off, and the account has been activated with an Iridium service provider. Systems
are generally shipped with a SIM card installed, with the PIN code disabled, and the
service inactive. The customer is responsible for this activation as the customer receives
the bills for the phone use. This process can take a day, and should be done in advance of
the installation/testing.
7.5
TRACKER SETUP
See the manual for the software to configure the unit to work as the customer
desires.
NOTE: This is a very important step in installing the system correctly,
DO NOT SKIP CONFIGURING THE TRACKER.
7.6
TRACKER TESTING
In order to fully test Tracker, you will need access to a PC running Sky Connect
Tracker-Map, or an approved GIS display system. In the event that this is not available to
you, contact Sky Connect Technical Support where we can remotely aid in your testing.
Refer to Appendix A for additional troubleshooting advice.
The Installer can verify the proper wiring of every onboard component with a
combination of the Tracker Setup program and the “all in one” annunciator light. The
Installer can be assured that their portion of the job is acceptable if the onboard unit
consistently indicates that it is sending and completing messages. (This is indicated by a
fast pulse as messages are sent at programmed intervals, followed by a solid green
indication.) It is the customer’s responsibility to choose the manner in which they display
their “tracked” aircraft, not the installers.
Note: Only one Iridium source can occupy the network at one time. If a Sky Connect
voice option is installed and in use, the Tracker will store and send position reports when
the line is free. Configurations will exist to give Tracker priority, thus
discontinuing an in-progress call. Alternatively, separate transceivers/antennae can be
used for multiple systems.
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Using ground power, turn on the Aircraft master, avionics master, or what ever is
required to fully power all elements of the installed Sky Connect components. If a G.P.S.
is interfaced, it must be operating and have acquired satellites. The aircraft must have an
unimpeded view of the sky. Operating next to a hangar can cause occasional brief signal
interruption of both G.P.S. and Iridium functionality. If using an internal G.P.S., allow
the unit to run for up to 15 minutes on the initial startup to allow the internal G.P.S. to
acquire almanac data. Allow one minute for the system to register on the iridium
network.
Within this registration time, Tracker will generate a start up message which will be sent
via the Iridium network to our switching network, and then to the mapping system. At
this time, (approximately 24 seconds after the message was generated) a data block will
be available to your Tracking Provider. With some software systems there may be a
delay up to 1 ½ minutes before the aircraft is seen on your GIS. Giving the G.P.S. a
destination waypoint, and if possible some speed, will send additional parameters to the
mapping system for display, including Destination, Speed, Altitude, Flight Plan, etc.
IMPORTANT - Using the TRACKER SETUP program, you can test
most of the features of the installation with the exception of the full
network test. Any contact closures that were installed for use with
Tracker can be tested at this time as well. No messages will be
compiled or sent while the Tracker Setup program is connected and
running. Messages will resume, roughly one minute after the program
is discontinued.
From the main page, you can verify the G.P.S. position, speed, and altitude. The units
IMEI # and G.P.S. input type are displayed when known. The Iridium Signal strength
(0-5) and Modem status are displayed and updated in real time.
From the Switch configuration page you can select the type and rate of each switch input,
but you can also test to verify the input. The Setup program samples the incoming
switches every ten seconds to see if they are active. The switch status will display as on if
a ground is applied to the corresponding pin, and off if the line is floating.
Each closure will also generate a specific event at the PC running the mapping system
software. The program must have an “assignment” for the event triggers to accomplish
their task. The assignment for contact closure #2, for example, can be assigned on the
mapping system PC terminal to annunciate “Mission Aborted.” The important element
here is that the contact closure number is accurate to the specific switch being tested.
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Purposes for these switches are defined by the end user. For more clarity on this
programming, refer to the mapping system operation manual.
Should you desire to use our Tech Support for these tests, you will need to have available
the Transceiver Serial Number, IMEI#, aircraft flight ID, and installed
options/configuration. With power applied, Tracker will continue to generate position
report updates at its programmed interval. Once registered on the network, Tracker
interval reports are billed per hour of use including during the testing process.
Note: Programmed interval directly affects customer billing. Consult
with end user regarding all available configuration options before
accomplishing.
7.7
7.7.1
OPERATION
TRACKER
The Sky Connect Tracker system consists of the transceiver and L-band antenna,
as well as an additional module in the transceiver. The Tracker can be added to
any system but works autonomously of them. The Tracker can utilize a feed from
most panel mounted G.P.S. systems, or its own internal G.P.S. (when equipped
with separate active G.P.S. antenna). This feed of aviation data provides Tracker
with aircraft flight parameters such as latitude, longitude, speed, direction,
altitude, and flight plan information if available.
The Tracker utilizes Short Burst Messaging over the Iridium network to send this
flight information packet to ground terminals for the monitoring of fleet aircraft.
Regular reporting intervals of twelve seconds to greater than 30 minutes can be set
for the triggering of a flight information packet. Three separate rates can be
selected based on flight status.
In addition to interval reporting, changes in flight parameters, proximity to
waypoint, or “events” can trigger reports. Events can be triggered by contact
closures, such as a squat switch, or an emergency button. DC level inputs may
require external diode protection. While no external switching or annunciation is
required for the Tracker system to operate, it can contain up to eight external
event switches, and four status annunciators. It is recommended that at least one
annunciator be installed in a suitable location which would provide verification of
a completed message transaction. This annunciator would alert the user to the
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system status and a reception (or lack thereof) of the flight information packet at
the Iridium Gateway.
7.7.4
MMU
See the MMU Operator’s Manual for a detail description of the MMU. The
MMU communicates with the transceiver over an RS-232 port. This is a three
wire port. The MMU is fully user configurable and offers a great deal of
flexibility to the system.
The MMU was designed to replace our legacy SOP Dialer to enhance the
functions offered to the SOP System.
The MMU can store 99 phone numbers with an alpha identifier to better detail
who you are dialing.
Operation is simple and standard with today’s digital avionics packages.
The MMU provides a user interface to an external Iridium transceiver, allowing a
user to control voice calls and send & receive text SBD messages. The MMU
contains a 2-line, 16 character alphanumeric display and a rotary knob with a
pushbutton action. External I/O includes an RS232 port.
The MMU is loaded with a “Message Set”, which is saved in Flash memory. The
Message Set contains configuration data, the names and phone number choices for
voice dialing, and the complete set of text messages that can be selected by the
user for transmission to the ground. The Message Set may be loaded on the
ground via the MMU’s RS232 port.
The MMU communicates with the map application via binary SBD messages.
Mobile Terminated (“MT”) messages are sent from the ground to the MMU, and
Mobile Originated (“MO”) messages are sent from the MMU to the ground.
These messages are sent to and from the Map.
Phone numbers and messages are created for the MMU by using a Sky Connect
program called MSETgen. This program will create a message set of phone
numbers and canned messages to be loaded into the MMU with its companion
program called MMUload. MMUload uses the RS-232 port to update the internal
software as well as load new message sets into the MMU.
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The MMU does not contain the switches found on the legacy SOP Dialer, but
those switches are offered by part number for parties interested in installing them
as an option. With this version of the MMU, the switches are wired to the
Transceiver.
The MMU supports driving two annunciators to indicate when a call is coming in
and when a message is incoming.
Send flight plan information using the G.P.S. data as To/From reference. FP data
will contain; TO/FROM waypoints, ETA, Number of PAX, and Fuel on Board in
Pounds.
The MMU will control the volume of the LBT through its serial port.
The MMU has a signal strength indicator in its display.
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8
TELEPHONE INDICATIONS and SETUP
8.1
TRANSCEIVER INDICATIONS
The Sky Connect Executive, Classic, and FlightDeck transceivers are equipped with
diagnostic lights on the side of the transceiver. The performance of these lights is very
important as an aid to diagnosing performance problems. This section describes the
purpose of each light.
On power up, all lights will come on briefly, followed by a blinking of the software
revision. Software major designator is indicated by the green Signal Strength bars, while
minor increment is indicated by the yellow bars. Two green flashes followed by three
yellow flashes indicates version 2.3.
Signal Strength—When registered with the network, these lights will indicate
your current signal strength by displaying zero to five bars. Anything less than
three bars will usually result in a failed call attempt. Signal strength changes as
azimuth to satellite changes. In the air, this will not have much effect. On the
ground, satellite azimuth can have you wondering why you have no reception, or
can’t register with the network. If on the ground, do not waste time, get as far
from the hangars as you can.
Signal strength is not indicated when in a data call. As a result, the signal strength
bars will alternate on and off (1,3, and 5, followed by 2, and 4). Throughout the
duration of a data call.
Ringer—This light will flash in a ringing cadence with any inbound call.
Power—This light will remain solid at all times that external power is applied
and the system is operational..
Off Hook—This light indicates when a Executive or FlightDeck phone is off
hook. When this light is on, you will hear dial tone, or busy signal in the handset
(or headset).
Data Call—This light indicates that DTR is high on the PC interface, and likely
that a data call is in progress. This light is coincident with the flashing Signal
Strength bars.
Voice Call—This light indicates that a Voice call has connected and is in
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progress.
Register—This light will blink while a unit is attempting to register with the
network. This process happens each time the unit is powered. The light will go
solid once registration has occurred. Registration implies that at some point, at
least one bar of signal strength was available for roughly ten seconds, though a
registered phone does not necessarily mean you currently have adequate signal
strength for a call. A registered unit means that a valid SIM card is installed, an
account is active with a service provider, and the Antenna subsystem is sufficient
to provide one bar of coverage. Until registered you will be unable to make or
receive calls.
SC1—Tracker transceivers, this light will reflect the operation of the Status light
on the SOP Dialer. Full Telephony transceivers like the Executive, this light has
no function.
8.2
PHONE TESTING (REF. CIL 2006-002 ON WEBSITE)
8.2.1
AIRCRAFT TO GROUND
Using ground power, turn on the Aircraft master, avionics master, or what ever is
required to fully power all elements of the installed Sky Connect system. The Iridium
antenna must have an unimpeded view of the sky. Operating next to a hangar can
cause occasional brief signal interruption. Allow at least one minute for the system to
register on the Iridium network.
Using the international country code, area code, and number, place a phone call (i.e.
001-301-891-0600#). If using an executive handset, you can test speaker mode at this
point as well.
8.2.2
GROUND TO AIRCRAFT
A call to the aircraft from the ground can be done in one of two ways;
1.)
2.)
call the aircraft number using the international code of 011-88-163-xxx-xxxx
where the xs are the given number.
Call the Iridium phone number 480-768-2500, and then dial the 88-163-xxx-xxxx
number. This option may not be available to all customers. Use of this option
depends on activation of this feature at time of purchase.
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The second example is cheaper for customers calling within the US, because it offers
Iridium users a special rate per minute.
Note: There are some inherent delays and audio quality degradation in
the use of satellite communications. These anomalies can come and
go depending on current azimuth to the satellite in use, and even
specific satellite characteristics.
Calls will occasionally be dropped due to momentary signal loss in
excess of 12 seconds. This sometimes frustrating characteristic is a
normal aspect of all wireless communications.
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9
APPENDIX A Troubleshooting
TROUBLESHOOTING THE SKY CONNECT SYSTEMS
Table 12
Description of Problem
Possible Causes
Executive, FlightDeck, Classic only
Unit has no external indication of
power
Check power and ground connections for
proper polarity, and to ensure no shorts or
opens.
Verify 11-33 VDC at the 62 pin connector.
Check connector seating.
Contact Technical Support
Power light comes on, but register light
remains blinking
Verify unit is outside, clear of obstructions
(hangars).
Check all antenna connections and cable.
Verify customers service plan is fully
activated with service provider.
Verify SIM Card PIN is deactivated.
Verify that Inmarsat system, if on aircraft is
deactivated or properly filtered.
Verify cable length and type is appropriate to
achieve not more than 3dB loss at 1.6 GHz.
Check antenna placement on aircraft to be
free of obstructions or shadowing.
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Description of Problem
Possible Causes
Executive handset reads “line in use.”
Another handset is off hook.
A data call is in progress.
Verify that the Transceiver is powered and
that the “off hook” light is off.
Check wiring between Transceiver and Base
Station for Intermittent opens or shorts of
Tip/Ring lines.
Executive handset keeps repeating 3
melodic tones when I go “off hook.”
A PIN code is still on the SIM card contact
tech support before any attempt to dial is
made.
Executive handset played 3 repeating
tones and my call attempts failed, even
though melodic I now hear a dial tone
instead of the 3 melodic tones.
A PIN code is still on the SIM card, and you
have locked the phone by entering invalid
codes.
Contact Technical Support
I dial numbers hear a pause, and then a
repetitive sound consisting of two quick
dial tones and a pause.
Hit a # to start the call sequence on
Executive/Flight-Deck systems.
I dial numbers, hear call progress tones
or a pause followed by a return to dial
tone.
Your call did not complete for some reason,
no socket
established, try again.
Check signal strength by dialing *4*
1 beep—no signal strength
6 beeps—full signal strength
Classic Handset says “Enter PIN”
A PIN code is still on the SIM card.
Contact tech support before any attempt to
dial is made.
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Description of Problem
Possible Causes
Classic Handset says “BLOCKED”
A PIN code is still on the SIM card, and you
have locked the phone by entering invalid
codes. Contact tech support.
All Systems with Voice
I can make calls out, but not to the
aircraft when calling from a land-line.
The dialing sequence is different.
Verify that you are dialing an international
access code followed by the Iridium number,
or that you are following the proper
Two-Stage-Dialing procedures.
Contact your Service Provider.
Tracker System light pulses, goes solid,
but continues to wink off.
It does not attempt to resend the
message immediately, but waits until
its scheduled interval to transmit again.
Valid G.P.S. input is not available.
Light continues to wink off.
Verify unit is outside, clear of obstructions
(hangars).
Last received G.P.S. information is viewable
in the
Tracker Setup Program.
Check all antenna connections and cable.
Check antenna placement on aircraft to be
free of
obstructions or shadowing.
Unit was connected with reverse
polarity and no longer operates, or
operates for a short time followed by
power loss.
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